Turbine vane external heat transfer [microform] : final report / prepared for National Aeronautics and Space Administration, NASA-Lewis Research Center.

NASA thesaurus headings: Airfoils - Film cooling - Heat transfer coefficients - Leading edges - Two dimensional boundary layer - Data acquisition - Graphs (Charts) - Navier-stokes equation - Prediction analysis techniques - Tables (Data) - Aerodynamic characteristics - Heat tr...

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Corporate Authors: United States. National Aeronautics and Space Administration, Lewis Research Center, General Motors Corporation. Allison Gas Turbine Division
Other Authors: Turner, E. R., Yang, R. J.
Format: Government Document Microfilm Book
Language:English
Published: Indianapolis, IN : [Washington, D.C.] : [Springfield, Va.] : Allison Gas Turbine Division, General Motors Corporation ; NASA ; [For sale by the National Technical Information Service], [1985]
Series:NASA contractor report ; NASA CR-174827.
NASA contractor report ; NASA CR-174828.
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Summary:NASA thesaurus headings: Airfoils - Film cooling - Heat transfer coefficients - Leading edges - Two dimensional boundary layer - Data acquisition - Graphs (Charts) - Navier-stokes equation - Prediction analysis techniques - Tables (Data) - Aerodynamic characteristics - Heat transfer - Turbine engines - Prediction analysis techniques - Flow distribution - Pressure measurement - Thermal boundary layer - Time dependence - Viscous flow.
Abstract:Research to improve the predictive design capabilities for external heat transfer to turbine vanes, including the ffects of leading edge showerhead film cooling. Vol. 1 describes the program conducted at Allison Gas Turbines to examine the effect of leading edge showerhead film cooling on downstream heat transfer. The study was performed in a two-dimensional linear cascade. In vol. 2, the application of the time-dependent ensemble-averaged Navier-Stokes equations to transonic turbine cascade flow fields was examined. In particular, efforts focused on an assessment of the procedure in conjunction with a suitable turbulence model to calculate steady turbine flow fields using an O-type coordinate system.
Item Description:"July 1985."
Physical Description:2 volumes : illustrations.
Distributed to depository libraries in microfiche; also available via the Internet.
Bibliography:Includes bibliographical references (volume 1, pages 232-233; volume 2, pages 149-153)
Reproduction Note:Microfiche.
Additional Physical Form available Note:Distributed to depository libraries in microfiche; also available via the Internet.
Funding Information Note:NASA contract no.